The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 13, 2020

Filed:

Feb. 27, 2017
Applicant:

Textron Innovations Inc., Providence, RI (US);

Inventors:

Christopher Mike Bothwell, Grapevine, TX (US);

Luke Dafydd Gillett, Grapevine, TX (US);

Jillian Samantha Alfred, Fort Worth, TX (US);

Assignee:

TEXTRON INNOVATIONS INC., Providence, RI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/50 (2006.01); G05D 1/00 (2006.01); B64C 27/57 (2006.01); B64C 13/28 (2006.01); B64C 13/10 (2006.01); F02C 9/28 (2006.01); F02C 9/58 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0055 (2013.01); B64C 13/10 (2013.01); B64C 13/343 (2018.01); B64C 13/345 (2018.01); B64C 13/507 (2018.01); B64C 27/57 (2013.01); F02C 9/28 (2013.01); F02C 9/58 (2013.01); F05D 2220/329 (2013.01); F05D 2270/021 (2013.01);
Abstract

A flight control computer (FCC) for a rotorcraft includes a processor and a non-transitory computer-readable storage medium storing a program to be executed by the processor, with the program including instructions for providing main rotor overspeed protection. The instructions for providing the main rotor overspeed protection include instructions for monitoring sensor signals indicating a main rotor RPM, determining a target operating parameter, determining one or more flight parameters in response to a relationship between the main rotor RPM and the target operating parameter indicating a main rotor overspeed condition. Determining the one or more flight parameters includes determining a setting for a flight control device of the rotorcraft that changes the main rotor RPM, controlling positioning of a pilot control according to the flight parameters, and controlling the flight control device of the rotorcraft according to positioning of the pilot control.


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